[Technical Field]
[0001] The present invention relates to a turbine stator, a steam turbine, and a partition
plate.
[Background Art]
[0003] A steam turbine includes a rotor that rotates centered on an axis and a casing that
covers the rotor. The rotor has a rotor shaft extending in an axial direction centered
on the axis, and a plurality of rotor blades disposed around the rotor shaft. In a
casing, a partition plate having a plurality of nozzles (stator blades) disposed around
the rotor is fixed to an upstream side of each rotor blade.
[0004] Patent Literature 1 discloses a nozzle diaphragm (partition plate) in which a nozzle
diaphragm outer ring (outer ring) is provided on an outer side of the nozzle in a
radial direction, and a nozzle diaphragm inner ring (inner ring) is provided on an
inner side of the nozzle. The nozzle diagram is formed in an annular shape by vertically
combining semi-annular members. Such a nozzle diaphragm accommodates the turbine rotor
inside in a rotatable state. A plurality of nozzle diaphragms are arranged in the
casing.
[Citation List]
[Patent Literature]
[Patent Literature 1]
[0005] Japanese Unexamined Patent Application, First Publication No.
2017-150386
[Summary of Invention]
[Technical Problem]
[0006] By the way, in the steam turbine, the steam flowing inside causes a pressure difference
between an upstream side and a downstream side of the partition plate in the axial
direction. Due to the pressure difference, a load is generated on the partition plate
so that the inner side in the radial direction bends toward the downstream side in
the axial direction. In order to suppress the deformation of the partition plate due
to such a load, the strength of the partition plate is maintained by ensuring a constant
thickness in the axial direction. On the other hand, in a case where the partition
plate is thick, there is a concern that the size of the steam turbine will increase
significantly as the number of stages increases. Therefore, it is desired that deformation
of the partition plate is suppressed while reducing the thickness in the axial direction.
[0007] The present invention provides a turbine stator, a steam turbine, and a partition
plate capable of suppressing deformation while reducing the thickness in the axial
direction.
[Solution to Problem]
[0008] A turbine stator according to a first aspect of the present invention includes a
partition plate including an inner ring that extends along a circumferential direction
around an axis, an outer ring that is disposed on an outer side with respect to the
inner ring in a radial direction with respect to the axis, and extends in the circumferential
direction, a plurality of nozzles that are disposed between the inner ring and the
outer ring in the circumferential direction, and are configured to guide a fluid from
an upstream side toward a downstream side in an axial direction in which the axis
extends, and an annular protruding portion, protrudes from the outer ring to the downstream
side in the axial direction, and extends along the outer ring in the circumferential
direction, and a casing surrounding the partition plate from the outer side in the
radial direction, and having a contact support surface that is in contact with the
annular protruding portion from the downstream side in the axial direction.
[0009] According to such a configuration, by the annular protruding portion and protrudes
from the outer ring, the partition plate has a shape in which a region on the outer
side in the radial direction protrudes to the downstream side so as to have an arch
shape when viewed from the radial direction. Further, the partition plate is supported
by the casing in a state where the annular protruding portion is in contact with the
contact support surface. As a result, a compressive force acts on a region of the
partition plate on the inner side in the radial direction. Even in a case where a
load is generated by the differential pressure between the upstream side and the downstream
side of the partition plate, the compressive force resists the load, so that in the
partition plate, deformation such that the region on the inner side in the radial
direction is directed to the downstream side in the axial direction is suppressed.
In this way, the rigidity of the partition plate with respect to the differential
pressure can be ensured without increasing the thickness of the region on the inner
side in the radial direction.
[0010] In the turbine stator according to a second aspect of the present invention, the
annular protruding portion may protrude to the outer side in the radial direction
from an outer circumferential surface of the outer ring facing the outer side in the
radial direction.
[0011] According to such a configuration, the annular protruding portion in the partition
plate contacts with the casing earlier than the outer ring and serves as a guide for
the casing. As a result, the position of the annular protruding portion with respect
to the casing can be determined with high accuracy. Accordingly, the annular protruding
portion can be reliably brought into contact with the contact support surface, and
the deformation of the partition plate can be suppressed with higher accuracy.
[0012] In the turbine stator according to a third aspect of the present invention, the annular
protruding portion may have a tapered surface formed at a corner that is formed by
a protruding portion outer circumferential surface facing the outer side in the radial
direction and a protruding portion upstream surface facing the upstream side in the
axial direction.
[0013] According to such a configuration, in a case where the upper half casing is assembled
to the partition plate, it is possible to prevent the inner circumferential surface
of the casing from being placed on the corner and making it difficult for the annular
protruding portion to fit. As a result, it is possible to suppress the assemblability
from being deteriorated such that the partition plate and the casing do not fit.
[0014] In the turbine stator according to a fourth aspect of the present invention, the
partition plate may include an upper half partition plate having a semi-annular shape,
and upper half partition plate dividing surfaces, which are horizontal surfaces facing
a lower side in a vertical direction, at both ends in the circumferential direction,
a lower half partition plate having a semi-annular shape, and lower half partition
plate dividing surfaces, which are configured to contact with the upper half partition
plate dividing surfaces, at both ends in the circumferential direction, and a fixing
unit fixing the upper half partition plate and the lower half partition plate to be
immovable at a position closer to the nozzle than at least one of the outer circumferential
surface of the outer ring and the outer circumferential surface of the annular protruding
portion in the radial direction.
[0015] According to such a configuration, it is possible to improve the assemblability of
the partition plate by having the vertically divided structure. Further, the upper
half partition plate and the lower half partition plate are fixed at the position
closer to the nozzle than at least one of the outer circumferential surface of the
outer ring or the outer circumferential surface of the annular protruding portion
in the radial direction. As a result, in a case where a load is generated on the partition
plate, it is possible to make it difficult to open the region on the inner side in
the radial direction, which is particularly easy to open, of the upper half partition
plate dividing surface and the lower half partition plate dividing surface. Accordingly,
the amount of deformation of the partition plate can be suppressed.
[0016] In the turbine stator according to a fifth aspect of the present invention, a fin
may be disposed on a surface of the annular protruding portion, which faces an inner
side in the radial direction.
[0017] According to such a configuration, the annular protruding portion itself can serve
as a flow guide.
[0018] A steam turbine according to a sixth aspect of the present invention includes the
turbine stator, and a rotor that is configured to rotate around the axis in the turbine
stator.
[0019] According to such a configuration, the thickness of the partition plate is reduced,
so that the size can be reduced. Further, even in a case where the number of stages
is increased to improve efficiency, the increase in size can be suppressed.
[0020] A partition plate according to a seventh aspect of the present invention includes
an inner ring that extends along a circumferential direction around an axis, an outer
ring that is disposed on an outer side with respect to the inner ring in a radial
direction with respect to the axis, and extends in the circumferential direction,
a plurality of nozzles that are disposed between the inner ring and the outer ring
in the circumferential direction, and are configured to guide a fluid from an upstream
side toward a downstream side in an axial direction in which the axis extends, and
a annular protruding portion, protrudes from the outer ring to the downstream side
in the axial direction, and extends along the outer ring in the circumferential direction,
in which the annular protruding portion protrudes to the outer side in the radial
direction from an outer circumferential surface of the outer ring facing the outer
side in the radial direction.
[Advantageous Effects of Invention]
[0021] According to the present invention, it is possible to suppress deformation while
reducing the thickness in the axial direction.
[Brief Description of Drawings]
[0022]
Fig. 1 is a cross-sectional view of a steam turbine according to an embodiment of
the present invention.
Fig. 2 is a cross-sectional view showing a cross section of a main part inside the
steam turbine according to the present embodiment.
Fig. 3 is a cross-sectional view showing a cross section of a main part inside a partition
plate according to the present embodiment.
Fig. 4 is a schematic view of the partition plate according to the present embodiment
as viewed from the axial direction.
[Description of Embodiments]
[0023] Hereinafter, a steam turbine 1 according to an embodiment of the present invention
will be described in detail with reference to the drawings.
[0024] As shown in Fig. 1, the steam turbine 1 includes a rotor 2 and a turbine stator 10.
[0025] The rotor 2 is rotatable around an axis Ar. The rotor 2 has a rotor shaft 21 extending
in an axial direction Da around the axis Ar, and a plurality of rotor blades 22 fixed
to the rotor shaft 21 along a circumferential direction Dc with respect to the rotor
shaft 21.
[0026] In the following, the direction in which the axis Ar extends is referred to as the
axial direction Da. The radial direction with respect to the axis Ar as a reference
is simply referred to as a radial direction Dr. In the radial direction Dr, the vertical
direction of the paper surface in Fig. 1 is defined as a vertical direction Dv. Further,
the right and left direction of Fig. 1 and the right and left direction of Fig. 4
are defined as a horizontal direction Dh orthogonal to the vertical direction Dv.
Further, the direction around the rotor 2 centered on the axis Ar is defined as the
circumferential direction Dc.
[0027] The turbine stator 10 accommodates the rotor 2 inside in a state of being rotatable
centered on the axis Ar. The turbine stator 10 has a partition plate 3 and a casing
4.
[0028] The partition plate 3 is disposed on the outer circumferential side of the rotor
2. The partition plate 3 has an annular shape centered on the axis Ar. The partition
plate 3 that has an annular shape has a plurality of nozzles (stator blades) 8 arranged
in the circumferential direction Dc at a position near the middle of the partition
plate 3 in the radial direction Dr and on the upstream side in the axial direction
Da from the rotor blade 22 of the rotor 2. In the steam turbine 1, a cylindrical space
on the outer circumferential side of the rotor shaft 21 and near the middle of the
partition plate 3 that has an annular shape, that is, the space where the rotor blade
22 and a nozzle 8 are disposed is a steam flow path through which steam of working
fluid flows. The details of the shape of the partition plate 3 will be described below.
[0029] The casing 4 is disposed on the outer circumferential side of the partition plate
3. The casing 4 has a cylindrical shape centered on the axis Ar. The casing 4 surrounds
the partition plate 3 from the outer side in the radial direction Dr. The casing 4
that has a cylindrical shape includes an upper half casing 41 on the upper portion
and a lower half casing 42 on the lower portion with the axis Ar of the rotor 2 as
a reference.
[0030] The upper half casing 41 extends in the circumferential direction Dc. The cross section
of the upper half casing 41 orthogonal to the axis Ar forms a semi-annular shape centered
on the axis Ar. The upper half casing 41 opens to face a lower side in the vertical
direction Dv so as to be capable of accommodating the rotor 2 and the partition plate
3.
[0031] The lower half casing 42 extends in the circumferential direction Dc. The cross section
of the lower half casing 42 orthogonal to the axis Ar forms a semi-annular shape centered
on the axis Ar. An inner diameter of the lower half casing 42 is formed to be the
same as an inner diameter of the upper half casing 41. The lower half casing 42 opens
to face the upper side in the vertical direction Dv so as to be capable of accommodating
the rotor 2 and the partition plate 3. The upper half casing 41 is placed on the lower
half casing 42 on the upper side in the vertical direction Dv and is fixed by a fastening
member such as a bolt 331 (not shown) in a state where the dividing surfaces are in
contact with each other. As a result, the casing 4 is formed.
[0032] As shown in Figs. 2 to 4, the partition plate 3 has an inner ring 6, an outer ring
7, the nozzle 8, and an annular protruding portion 9. The inner ring 6, the outer
ring 7, the nozzle 8, and the annular protruding portion 9 are integrally formed or
welded and joined to form a single member.
[0033] The inner ring 6 extends in the circumferential direction Dc around axis Ar. The
nozzle 8 is fixed to an inner ring outer circumferential surface 61, which is a surface
(outer circumferential surface) of the inner ring 6 facing the outer side in the radial
direction Dr. Specifically, an inner ring nozzle fixing groove 62 into which part
of the nozzle 8 is fitted is formed on the inner ring outer circumferential surface
61. The inner ring nozzle fixing groove 62 is a groove formed so as to be recessed
to the inner side in the radial direction Dr from the inner ring outer circumferential
surface 61. On the other hand, a seal support groove 64 supports a labyrinth seal
65 is formed on an inner ring inner circumferential surface 63, which is a surface
(inner circumferential surface) of the inner ring 6 facing the inner side of the radial
direction Dr. The seal support groove 64 is a groove formed so as to be recessed to
the outer side in the radial direction Dr from the inner ring inner circumferential
surface 63. That is, the seal support groove 64 opens to the inner side in the radial
direction Dr. The labyrinth seal 65 is a seal member made of, for example, an alloy
containing copper. The labyrinth seal 65 seals between the rotor shaft 21 and the
outer circumferential surface.
[0034] The outer ring 7 is provided on the outer side of the inner ring 6 in the radial
direction Dr such that the nozzle 8 is interposed. The outer ring 7 extends in the
circumferential direction Dc centered on the axis Ar. The nozzle 8 is fixed to an
outer ring inner circumferential surface 71, which is a surface (inner circumferential
surface) of the outer ring 7 facing the inner side in the radial direction Dr. Specifically,
an outer ring nozzle fixing groove 72 into which part of the nozzle 8 is fitted is
formed on the outer ring inner circumferential surface 71. The outer ring nozzle fixing
groove 72 is a groove formed so as to be recessed to the outer side in the radial
direction Dr from the outer ring inner circumferential surface 71.
[0035] The nozzle 8 is capable of guiding the fluid toward the rotor blade 22 from the upstream
side to the downstream side in the axial direction Da. A plurality of the nozzles
8 are provided in the circumferential direction Dc in a state of being interposed
between the inner ring 6 and the outer ring 7 in the radial direction Dr. The nozzle
8 according to the present embodiment has an inner shroud ring 81, a blade 82, and
an outer shroud ring 83.
[0036] As shown in Fig. 2, the inner shroud ring 81 fixes the blade 82 to the inner ring
6. An inner protrusion 811 that fits into the inner ring nozzle fixing groove 62 is
formed on the surface (inner circumferential surface) of the inner shroud ring 81
facing the inner side in the radial direction Dr. As shown in Fig. 3, in a state where
the inner protrusion 811 is fitted into the inner ring nozzle fixing groove 62, a
welding portion 50 is formed by performing welding between the inner shroud ring 81
and the inner ring 6 and is integrally joined.
[0037] As shown in Fig. 2, the outer shroud ring 83 fixes the blade 82 to the outer ring
7. The surface (inner circumferential surface) of the outer shroud ring 83 facing
the inner side in the radial direction Dr is integrated with an end portion of the
blade 82 on the outer side in the radial direction Dr. An outer protrusion 831 that
fits into the outer ring nozzle fixing groove 72 is formed on the surface (outer circumferential
surface) of the outer shroud ring 83 facing the outer side in the radial direction
Dr. As shown in Fig. 3, in a state where the outer protrusion 831 is fitted into the
outer ring nozzle fixing groove 72, the welding portion 50 is formed by performing
welding between the outer shroud ring 83 and the outer ring 7, and is integrally joined.
[0038] As shown in Fig. 2, the blade 82 extends between the inner shroud ring 81 and the
outer shroud ring 83 in the radial direction Dr. The blade 82 is a member having a
wing shape in cross-sectional shape as viewed from the radial direction Dr. The blade
82 and the rotor blade 22 described above are disposed at positions where the blade
82 and the rotor blade 22 overlap each other as viewed from the axial direction Da.
As shown in Fig. 4, a plurality of the blades 82 are disposed at intervals in the
circumferential direction Dc.
[0039] The annular protruding portion 9 extends in the circumferential direction Dc along
the outer ring 7. As shown in Fig. 2, the annular protruding portion 9 protrudes from
the outer ring 7 to the downstream side in the axial direction Da such that the position
of the axial direction Da overlap the rotor blade 22 disposed on the downstream side
of the nozzle 8 in a state where the partition plate 3 is accommodated in the casing
4. The annular protruding portion 9 is formed as an integral part with the outer ring
7. The annular protruding portion 9 according to the present embodiment protrudes
to the outer side in the radial direction Dr from the outer ring outer circumferential
surface 73 of the outer ring 7 in addition to the downstream side in the axial direction
Da. The outer ring outer circumferential surface 73 is the surface (outer circumferential
surface) of the outer ring 7 facing the outer side in the radial direction Dr. Further,
the annular protruding portion 9 also protrudes to the inner side in the radial direction
Dr from the outer ring inner circumferential surface 71. The annular protruding portion
9 protrudes to the position where the inner position in the radial direction Dr overlaps
the outer shroud ring 83 and does not overlap the blade 82 as viewed from the axial
direction Da. Therefore, the annular protruding portion 9 is formed in a size that
covers the outer ring 7 as viewed from the downstream side in the axial direction
Da. The annular protruding portion 9 has a protruding portion outer circumferential
surface 91, a protruding portion upstream surface 92, a protruding portion downstream
surface 93, and a protruding portion inner circumferential surface 94.
[0040] The protruding portion outer circumferential surface 91 is a curved surface of the
annular protruding portion 9 facing the outer side in the radial direction Dr. The
protruding portion outer circumferential surface 91 is formed on the outer side in
the radial direction Dr from the outer ring outer circumferential surface 73.
[0041] The protruding portion upstream surface 92 is a plane facing the upstream side in
the axial direction Da on the outer side in the radial direction Dr from the outer
ring outer circumferential surface 73. The protruding portion upstream surface 92
is formed on the upstream side of the protruding portion outer circumferential surface
91 in the axial direction Da. In the present embodiment, a tapered surface 921 is
formed on a corner formed by the protruding portion outer circumferential surface
91 and the protruding portion upstream surface 92. The tapered surface 921 is inclined
so as to face the upstream side in the axial direction Da and the outer side in the
radial direction Dr.
[0042] The protruding portion downstream surface 93 is a plane of the annular protruding
portion 9 facing the downstream side in the axial direction Da. The protruding portion
downstream surface 93 is connected to an end portion of the protruding portion outer
circumferential surface 91 on the downstream side in the axial direction Da. The protruding
portion downstream surface 93 is a surface parallel to the protruding portion upstream
surface 92 and facing the opposite side in the axial direction Da from the protruding
portion upstream surface 92.
[0043] The protruding portion inner circumferential surface 94 is a curved surface of the
annular protruding portion 9 facing the inner side in the radial direction Dr. The
end portion of the protruding portion inner circumferential surface 94 on the downstream
side in the axial direction Da is connected to the inner side of the protruding portion
downstream surface 93 in the radial direction Dr. The protruding portion inner circumferential
surface 94 is formed at a position at a distance from the end surface formed at the
tip of the rotor blade 22. A plurality of fins 941 are provided on the protruding
portion inner circumferential surface 94. Therefore, the protruding portion inner
circumferential surface 94 faces the outer end surface of the rotor blade 22 in the
radial direction Dr with a slight gap through the fins 941. As a result, the annular
protruding portion 9 also serves as a flow guide that guides the direction in which
steam flows.
[0044] As shown in Fig. 4, the partition plate 3 that has an annular shape includes an upper
half partition plate 31 on the upper portion in the vertical direction Dv and a lower
half partition plate 32 on the lower portion with the axis Ar of the rotor 2 as a
reference, and a fixing unit 33 that fixes the upper half partition plate 31 and the
lower half partition plate 32. The upper half partition plate 31 and the lower half
partition plate 32 each have the inner ring 6, the outer ring 7, the nozzle 8, and
the annular protruding portion 9.
[0045] The cross section of the upper half partition plate 31 orthogonal to the axis Ar
forms a semi-annular shape centered on the axis Ar. The upper half partition plate
31 opens to face the lower side in the vertical direction Dv such that the rotor 2
fits. The upper half partition plate 31 has upper half partition plate dividing surfaces
311 at both ends in the circumferential direction Dc. The upper half partition plate
dividing surface 311 is a horizontal surface facing the lower side in the vertical
direction Dv.
[0046] The lower half partition plate 32 extends in the circumferential direction Dc. The
lower half partition plate 32 is fixed to the lower half casing 42 in a state of being
accommodated inner side the lower half casing 42. The cross section of the lower half
partition plate 32 orthogonal to the axis Ar forms a semi-annular shape centered on
the axis Ar. The lower half partition plate 32 opens to face the upper side in the
vertical direction Dv such that the rotor 2 fits. The lower half partition plate 32
has lower half partition plate dividing surfaces 321 at both ends in the circumferential
direction Dc. The lower half partition plate dividing surface 321 is a horizontal
surface facing the upper side in the vertical direction Dv. The upper half partition
plate 31 is fixed by the fixing unit 33 in a state of being placed on the lower half
partition plate 32 on the upper side in the vertical direction Dv. As a result, the
partition plate 3 is formed.
[0047] The fixing units 33 are provided at two locations separated from each other in the
horizontal direction Dh. Here, the fixing unit 33 provided on one side of the horizontal
direction Dh on the right side of the paper surface in Fig. 4 will be described as
an example. The fixing unit 33 on the other side of the horizontal direction Dh, for
which description is omitted, also has the same configuration.
[0048] The fixing unit 33 fixes the upper half partition plate 31 and the lower half partition
plate 32 in a state where the upper half partition plate dividing surface 311 and
the lower half partition plate dividing surface 321 are in contact with each other.
Specifically, the fixing unit 33 fixes the annular protruding portion 9 of the upper
half partition plate 31 and the annular protruding portion 9 of the lower half partition
plate 32 immovably at a position closer to the nozzle 8 than the protruding portion
outer circumferential surface 91 in the radial direction Dr. The fixing unit 33 according
to the present embodiment includes the bolt 331, a bolt insertion recess 332 formed
in the upper half partition plate 31, and a bolt fixing unit 333 formed in the lower
half partition plate 32.
[0049] The bolt insertion recess 332 is recessed in the vertical direction Dv so as to be
toward the upper half partition plate dividing surface 311 from the outer circumferential
surface (outer ring outer circumferential surface 73) of the upper half partition
plate 31. The bolt insertion recess 332 forms a bolt contact surface 332a that is
in contact with a head portion of the bolt 331. The bolt contact surface 332a is formed
at a position separated from the upper half partition plate dividing surface 311 in
the vertical direction Dv. The bolt contact surface 332a is a plane parallel to the
upper half partition plate dividing surface 311. A bolt insertion hole 332b in which
a screw portion of the bolt 331 can be inserted is formed in the bolt contact surface
332a. The bolt insertion hole 332b penetrates the upper half partition plate 31 from
the bolt contact surface 332a to upper half partition plate dividing surface 311.
[0050] The bolt fixing unit 333 is a screw hole recessed from the lower half partition plate
dividing surface 321. The bolt fixing unit 333 is capable of fixing the bolt 331 by
inserting the screw portion of the bolt 331. The bolt fixing unit 333 is provided
at a position closer to the outer circumferential surface of the outer shroud ring
83 than the protruding portion outer circumferential surface 91 in the radial direction
Dr. The bolt fixing unit 333 is formed such that the position of in the radial direction
Dr and the axial direction Da coincides with the bolt insertion hole 332b.
[0051] As shown in Fig. 2, a plurality of casing positioning recesses 45 recessed over the
entire circumference are formed in the inner circumferential surface of the casing
4. The annular protruding portion 9 can be inserted into the casing positioning recess
45. As a result, the casing positioning recess 45 determines the position of the partition
plate 3 in the axial direction Da with respect to the casing 4. The casing positioning
recess 45 has a recess separation surface 451, a recess bottom surface 452, and a
contact support surface 453.
[0052] The recess separation surface 451 extends vertically from the inner circumferential
surface of the casing 4. The recess separation surface 451 is a plane facing the protruding
portion upstream surface 92. The recess separation surface 451 is formed at a position
spaced apart from the protruding portion upstream surface 92 in a state where the
partition plate 3 is accommodated in the casing 4.
[0053] The recess bottom surface 452 is a surface forming a bottom portion of the recess.
The recess bottom surface 452 faces the inner side in the radial direction Dr. The
recess bottom surface 452 is a surface parallel to the inner circumferential surface
of the casing 4. The recess bottom surface 452 extends vertically from the end portion
of the recess separation surface 451 on the outer side in the radial direction Dr.
The recess bottom surface 452 is a surface facing the protruding portion outer circumferential
surface 91. The recess bottom surface 452 is formed at a position spaced apart from
the protruding portion outer circumferential surface 91 in a state where the partition
plate 3 is accommodated in the casing 4.
[0054] The contact support surface 453 extends vertically from the inner circumferential
surface of the casing 4. The contact support surface 453 connects the inner circumferential
surface of the casing 4 and the end portion of the recess bottom surface 452 on the
downstream side in the axial direction Da. In the casing positioning recess 45, the
contact support surface 453 faces the recess separation surface 451. The contact support
surface 453 is a plane parallel to the recess separation surface 451. The contact
support surface 453 faces the protruding portion downstream surface 93. The contact
support surface 453 is formed at a position being in contact with the protruding portion
downstream surface 93 in a state where the partition plate 3 is accommodated in the
casing 4. That is, the contact support surface 453 is in contact with the annular
protruding portion 9 from the downstream side in the axial direction Da.
[0055] According to the turbine stator 10 described above, the annular protruding portion
9 is formed integrally with the outer ring 7 and protrudes to the downstream side
in the axial direction Da from the outer ring 7. As a result, the partition plate
3 has a shape in which the region on the outer side in the radial direction Dr protrudes
to the downstream side in the axial direction Da from the region on the inner side
in the radial direction Dr where the nozzle 8 or the inner ring 6 is disposed so as
to have an arch shape when viewed from the radial direction Dr. Here, in the steam
turbine 1, due to the influence of the steam flowing inside, the pressure with respect
to the partition plate 3 on the downstream side in the axial direction Da is lower
than the pressure on the upstream side. Due to the differential pressure between the
upstream side and the downstream side of the partition plate 3, a load is generated
on the partition plate 3 such that the region on the inner side in the radial direction
Dr is curved toward the downstream side in the axial direction Da. However, in the
partition plate 3 according to the present embodiment, the region on the outer side
in the radial direction Dr protrudes to the downstream side in the axial direction
Da. Further, the partition plate 3 is supported by the casing 4 in a state where the
protruding portion downstream surface 93 is in contact with the contact support surface
453. As a result, a compressive force acts on the region of the partition plate 3
on the inner side in the radial direction Dr. Even in a case where a load is generated
by the differential pressure between the upstream side and the downstream side of
the partition plate 3, the compressive force resists the load, so that in the partition
plate 3, deformation such that the region on the inner side in the radial direction
Dr is directed to the downstream side in the axial direction Da is suppressed. As
a result, the rigidity of the partition plate 3 with respect to the differential pressure
can be ensured without increasing the thickness of the region on the inner side in
the radial direction Dr. Therefore, it is possible to suppress the deformation of
the partition plate 3 while reducing the thickness of the partition plate 3 in the
axial direction Da.
[0056] Also, the annular protruding portion 9 protrudes to the outer side of the outer ring
7 in the radial direction Dr in addition to the axial direction Da. Therefore, in
a case where the upper half casing 41 is assembled to the partition plate 3 accommodated
in the lower half casing 42, the annular protruding portion 9 first contacts with
the upper half casing 41 in the partition plate 3, and becomes a guide with respect
to the upper half casing 41. As a result, the position of the annular protruding portion
9 with respect to the casing 4 can be determined with high accuracy. Accordingly,
the annular protruding portion 9 can be reliably brought into contact with the contact
support surface 453, and the deformation of the partition plate 3 can be suppressed
with higher accuracy.
[0057] Further, the tapered surface 921 is formed on the corner formed by the protruding
portion upstream surface 92 and the protruding portion outer circumferential surface
91. Therefore, in a case where the upper half casing 41 is assembled to the partition
plate 3, it is possible to prevent the inner circumferential surface of the casing
4 from being placed on the corner and making it difficult for the annular protruding
portion 9 to be inserted into the casing positioning recess 45. Therefore, the annular
protruding portion 9 can be smoothly inserted into the casing positioning recess 45.
As a result, it is possible to suppress the assemblability from being deteriorated
such that the partition plate 3 and the casing 4 do not fit.
[0058] Further, the annular protruding portion 9 also protrudes to the inner side of the
outer ring 7 in the radial direction Dr. Further, the fins 941 that are sliding contact
with the tip of the rotor blade 22 are provided on the protruding portion inner circumferential
surface 94. Therefore, the annular protruding portion 9 itself can serve as a flow
guide.
[0059] Also, since the partition plate 3 has the vertically divided structure, it is possible
to improve the assemblability of the partition plate 3. On the other hand, in a case
where a load is generated on the partition plate 3 due to the vertically divided structure,
the upper half partition plate 31 and the lower half partition plate 32 are easily
deformed so as to be open between the upper half partition plate dividing surface
311 and the lower half partition plate dividing surface 321. However, the bolt fixing
unit 333 is formed at a position closer to the outer circumferential surface of the
outer shroud ring 83 than the protruding portion outer circumferential surface 91
in the radial direction Dr.
Therefore, the upper half partition plate 31 and the lower half partition plate 32
are fixed at positions close to the nozzle 8. As a result, in a case where a load
is generated on the partition plate 3, it is possible to make it difficult to open
the region on the inner side in the radial direction Dr, which is particularly easy
to open, of the upper half partition plate dividing surface 311 and the lower half
partition plate dividing surface 321. Accordingly, the amount of deformation of the
partition plate 3 can be suppressed.
[0060] Further, by using the partition plate 3 having the annular protruding portion 9,
the thickness of the partition plate 3 is reduced. Therefore, the casing 4 can be
made smaller than the case where the partition plate 3 having no annular protruding
portion 9 is used. In particular, in the present embodiment, the position of the annular
protruding portion 9 in the axial direction Da overlaps the position of the rotor
blade 22. Therefore, the annular protruding portion 9 is formed by utilizing the space
located on the outer side of the rotor blade 22 in the radial direction Dr. As a result,
in the partition plate 3, the thickness of the region on the inner side in the radial
direction Dr (the region adjacent to the rotor blade 22 in the axial direction Da)
where the nozzle 8 or the inner ring 6 is formed can be prevented from increasing.
As a result, the steam turbine 1 as a whole can be made compact. Further, even in
a case where the number of stages is increased to improve efficiency of the steam
turbine 1, the increase in size of the steam turbine 1 as a whole can be prevented.
(Modification Example Other Than Embodiment)
[0061] Although the embodiments of the present invention have been described in detail with
reference to the drawings, the configurations and combinations thereof in the respective
embodiments are examples, and the configurations are added, omitted, replaced, and
changed within a range not deviating from the gist of the present invention. Further,
the present invention is not limited to the embodiment, but only to the scope of claims.
[0062] For example, the annular protruding portion 9 is not limited to being formed integrally
with the outer ring 7. The annular protruding portion 9 need only have a structure
in which the protruding portion downstream surface 93 is in contact with the casing
4 while protruding to the downstream side in the axial direction Da from the outer
ring 7. Therefore, the annular protruding portion 9 may be joined to the outer ring
7 by welding or the like after being formed by a member different from the outer ring
7.
[0063] Further, the annular protruding portion 9 is not limited to have a structure in which
the fins 941 are provided on the protruding portion inner circumferential surface
94. For example, the annular protruding portion 9 has a structure that does not protrude
to the inner side in the radial direction Dr from the outer ring 7, and a flow guide
provided with the fins separately from the annular protruding portion 9 may be disposed
between the annular protruding portion 9 and the rotor blade 22 in the radial direction
Dr.
[0064] Also, the fixing unit 33 is not limited to have a structure of immovably fixing the
annular protruding portion 9 of the upper half partition plate 31 and the annular
protruding portion 9 of the lower half partition plate 32 at a position closer to
the nozzle 8 than the protruding portion outer circumferential surface 91 in the radial
direction Dr. For example, in the case of the structure in which the annular protruding
portion 9 does not protrude to the outer side of the outer ring 7 in the radial direction
Dr, the fixing unit 33 may fix the upper half partition plate 31 and the lower half
partition plate 32 at a position closer to the nozzle 8 than the outer circumferential
surface of the outer ring 7 in the radial direction Dr. Further, the fixing unit 33
is not limited to have a structure of fixing the annular protruding portion 9 of the
upper half partition plate 31 and the annular protruding portion 9 of the lower half
partition plate 32. The fixing unit 33 may fix the outer ring 7 of the upper half
partition plate 31 and the outer ring 7 of the lower half partition plate 32.
[Industrial Applicability]
[0065] According to the present invention, it is possible to suppress deformation while
reducing the thickness in the axial direction.
[Reference Signs List]
[0066]
1 steam turbine
2 rotor
21 rotor shaft
22 rotor blade
Ar axis
Da axial direction
Dr radial direction
Dv vertical direction
Dh horizontal direction
Dc circumferential direction
10 turbine stator
3 partition plate
6 inner ring
61 inner ring outer circumferential surface
62 inner ring nozzle fixing groove
63 inner ring inner circumferential surface
64 seal support groove
65 labyrinth seal
7 outer ring
71 outer ring inner circumferential surface
72 outer ring nozzle fixing groove
73 outer ring outer circumferential surface
8 nozzle
81 inner shroud ring
811 inner protrusion
82 blade
83 outer shroud ring
831 outer protrusion
50 welding portion
9 annular protruding portion
91 protruding portion outer circumferential surface
92 protruding portion upstream surface
921 tapered surface
93 protruding portion downstream surface
94 protruding portion inner circumferential surface
941 fin
31 upper half partition plate
311 upper half partition plate dividing surface
32 lower half partition plate
321 lower half partition plate dividing surface
33 fixing unit
331 bolt
332 bolt insertion recess
332a bolt contact surface
332b bolt insertion hole
333 bolt fixing unit
4 casing
41 upper half casing
42 lower half casing
45 casing positioning recess
451 recess separation surface
452 recess bottom surface
453 contact support surface